Attitude fuzzy logic controller design of a staring-imaging satellite in LEO

Author

Liang, HaiZhao ; Sun, Zhaowei ; Wu, Xiande

Author_Institution

Res. Centre of Satellite Technol., Harbin Inst. of Technol., Harbin, China

fYear

2009

fDate

9-12 Aug. 2009

Firstpage

762

Lastpage

766

Abstract

A fuzzy logic controller is designed for the attitude control of a staring-imaging satellite in LEO. The attitude kinematic and dynamic equations based-on Euler-Angle representations are developed; then, a FLC (Fuzzy Logic Control) law is designed for a staring-imaging satellite; finally, the simulations are performed. Comparing with traditional control methods, the method proposed here has quick convergence and robustness.

Keywords

artificial satellites; attitude control; control system synthesis; convergence; fuzzy control; stability; Euler-Angle representation; LEO; attitude control; attitude dynamic equation; attitude kinematic equation; convergence; fuzzy logic controller design; robustness; staring-imaging satellite; Attitude control; Design automation; Fuzzy logic; Kinematics; Low earth orbit satellites; Mechatronics; Optical sensors; Orbital calculations; Satellite ground stations; Sun; attitude control; controller design; fuzzy logic control; low earth orbit; staring image;

fLanguage

English

Publisher

ieee

Conference_Titel

Mechatronics and Automation, 2009. ICMA 2009. International Conference on

Conference_Location

Changchun

Print_ISBN

978-1-4244-2692-8

Electronic_ISBN

978-1-4244-2693-5

Type

conf

DOI

10.1109/ICMA.2009.5246203

Filename

5246203